This report has been prepared to present preliminary information relative to the flight of Mercury/Atlas MA-2 67D. The information presented is based on visual observation and data evaluation to the extent permitted by time limitations. It should be considered as preliminary only and the final reports on this flight referenced for further information. The technical content has been prepared and jointly agreed upon by members of the Mercury Launch Coordination Committee. (Author)
Mercury Launch Coordination Committee: Flight Test Report on Mercury/Atlas MA-2 (Atlas 67D), 21 February 1961, AMR Range Test Number 419, Convair Test Number P4-402-00-67
1961
72 pages
Report
No indication
English
Space Launch Vehicles & Support Equipment , Spacecraft Trajectories & Flight Mechanics , Launch vehicles , Flight testing , Payload , Reentry vehicles , Heat shields , Liquid propellant rocket engines , Hydraulic equipment , Pneumatic devices , Electrical equipment , Flight control systems , Guided missile safety , Propellant transfer , Impact prediction , Propellant control , Inertial guidance , Telemeter systems , Performance(Engineering) , Reliability(Electronics) , Atlas launch vehicles , Azusa , Ma-2 propulsion systems , Mercury project